N105ML, cancelled May 15, 2001

Service difficulty reports · 17

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N105ML' AND deregistration_id = 'N105ML-2001-05-15'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR JBXA000275Valve · out of adjUPON GEAR RETRACTION LEFT GEAR REMAINED DOWN WOULD NOT RETRACT. REINSPECTED AIR/GROUND TEST VALVE FOUND VALVE JUST OFF OF DETENT. REPOSITIONED TEST VALVE IN THE FULL FLIGHT DETENT AND SAFETIED VALVE IAW AMM 32-00-00-710-813A.Apr 29, 2001 · N105ML · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR JBXA000220Uplock Sensor · failedUPON LANDING AT LGA GEAR UNSAFE MESSAGE ILLUMINATED WHEN GEAR HANDLE WAS SELECTED TO THE DOWN POSITION. CYCLED GEAR HANDLE AND LIGHT WENT OUT. A/C WAS INSPECTED AND GEAR PINS INSTALLED. A/C WAS THEN FERRIED TO RDU. MX REPLACED THE RIGHT MLG UPLOCK SENSOR IANov 22, 2000 · N105ML · Fokker F28MK0100 · Landing Gear Position and WarningSDR JBXA0000192Valve · failedRETURNED TO RDU DUE TO FUEL VENTING OVERBOARD ON RT WING. REMOVED AND REPLACED RT WING TANK OVERFLOW VALVE IAW AMM 28-21-07. OPS CHECK AND LEAK CHECK GOOD.Jul 30, 2000 · N105ML · Fokker F28MK0100 · Aircraft Fuel Distribution SystemSDR JBXA0000160Sequence Valve · malfunctionedNOSE GEAR DID NOT EXTEND ON FIRST ATTEMPT. ON SECOND ATTEMPT IT EXTENDED NORMALLY. INSPECTED AIRCRAFT, PINNED GEAR AND PERFORMED MX FERRY FLIGHT IAW MIDWAY AIRLINES GMM CHAPTER 6 SECTION 4 FROM TPA TO RDU. REMOVED AND REPLACED NLG DOOR SEQUENCING VALVE AND Mar 28, 2000 · N105ML · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR JBXA0000153Uplock · malfunctionedAFTER TAKEOFF, THE LT MAIN LG DOOR AND RT MAIN LG DOOR SHOWED OPEN ON THE MFDU. RECYCLED THE LANDING GEAR WHICH WAS UNSUCCESSFUL IN CLEARING THE INDICATION ON THE MFDU. THE BLUE LIGHT IN THE GEAR HANDLE WAS ON WITH THE LANDING GEAR SELECTED UP AND OFF WITH TMar 14, 2000 · N105ML · Fokker F28MK0100 · Landing Gear SystemSDR JBXA0000152Selector Valve · malfunctionedUPON SELECTING GEAR DOWN, RIGHT MAIN DID NOT GET A DOWN AND LOCKED INDICATION (RECIEVED LEVEL THREE ALERT). CYCLED GEAR AND BOTH MAIN GEAR DID NOT DOWN AND LOCK. EXECUTED MISSED APPROACH. CYCLED GEAR AGAIN AND GOT THREE GREEN, LANDED NORMALLY. REMOVED AND Mar 13, 2000 · N105ML · Fokker F28MK0100 · Main Landing GearSDR JBXA0000138Valve · contaminatedFLIGHT NR 119 FLL TO RDU AIR RETURNED BLEED NR 1 AND NR 2 FAULTED AT 5000 FEET. WOULD NOT RESET IN FLIGHT. CLEANED NR 1 AND NR 2 ENGINE BLEED AIR MUSCLE SHUTTLE VALVES AND 80 PERCENT SWITCHES ON ENGINE NR 1 AND NR 2 OPS CHECK GOOD AT THIS TIME IAW AMM 36-11-Jan 13, 2000 · N105ML · Fokker F28MK0100 · Pneumatic Distribution SystemSDR JBXA9900122Bleed Air · failedBLEED 1 AND BLEED 2 FAULTED ON TAKEOFF AT 60 KNOTS. ABORTED TAKEOFF. ACCOMPLISHED CHECK PER MM 36-00-5, OPS CK GOOD.Nov 8, 1999 · N105ML · Fokker F28MK0100 · Pneumatic Distribution SystemSDR JBXA9900120Comm Sys · trippedFLIGHT 119 FROM FLL TO RDU, ON CLIMBOUT NR 1 AUDIO FAILED AND BACK-UP SYSTEM DID NOT WORK, COMPLETE COM FAILURE. RESET NR 1 AMU AND NR 2 AMU AND ALT AMU. PERFORMED OPERATIONAL CHECK IAW F-100 MM 23-51-00, OPERATIONAL CHECK GOOD. RESET NR 1 AND NR 2 VHF COMSNov 3, 1999 · N105ML · Fokker F28MK0100 · Communications SystemSDR JBXA9900104Bleed Valve · failedON CLIMB-OUT FROM RDU ON FLT 859, CREW REPORTED BLEED NR 1 AND 2 AND APU BLEED FAULTS. REMOVED AND REPLACED NR 2 HIGH PRESS BLEED VALVE IAW 36-11-00, OPS CHECK GOOD. ALSO, PERFORMED FUNCTIONAL CHECK FLT, ALL OPS CHECKED GOOD.Sep 9, 1999 · N105ML · Fokker F28MK0100 · APU Bleed Air SystemSDR JBXA9900103Switch · failedFLT 220 RDU/MCO ON CLIMBOUT HAD A RUDDER NR 2 FAULT. AIR RETURN TO RDU. PERFORMED OPS CHECK OF RLMU IAW 27-23-01, NO FAULTS NOTED ON GROUND. GROUND OPERATED ENGS AND PUT RUDDER IN SEVERAL CONFIGURATION AND NO FAULTS FOUND. REMOVED AND REPLACED ACTIVE RUDDESep 9, 1999 · N105ML · Fokker F28MK0100 · Rudder Control SystemSDR JBXA9900105Bleed Air Contl · out of adjustBOS- FLIGHT 668 ABORTED TAKEOFF, BLEED 1 AND 2 FAULT. NO RESET. ACCOMPLISHED BLEED AIR SUPPLY AND CONTROL. ADJUSTMENT AND TEST PER FOKKER 100 MM, CK'S OK PER 36-11-00.Sep 7, 1999 · N105ML · Fokker F28MK0100 · Pneumatic Distribution SystemSDR JBXA9900102Prsov · failedFLT NR 668 RDU/MCO ON CLIMB-OUT HAD BLEED 1 AND 2 FAULT AND PRESS CONTROLLER FAULT ON MFDU. RETURN TO RDU AND RETURNED TO THE GATE. REMOVED AND REPLACED NR 1 AND NR 2 PROSV. OPERATIONAL AND LEAK CHECKS ARE GOOD IAW F-100 MM 36-11-05. ALSO, PERFORMED SELF TSep 2, 1999 · N105ML · Fokker F28MK0100 · Cabin Pressure Control SystemSDR JBXA9900100Wheel · crackedON TAXI OUT CREW FELT SHIMMY IN TAIL OF AIRCRAFT. MAINTENANCE INSPECTED AND FOUND OUTER WHEEL BEARING JOURNAL ON NR 3 MAIN WHEEL HEAT DAMAGED AS A RESULT OF WHEEL FAILURE. MAINTENANCE REMOVED AND REPLACED NR 3 AND NR 4 MAIN WHEEL ASSY AND REMOVED AND REPLACEAug 21, 1999 · N105ML · Fokker F28MK0100 · Wheel/Ski/FloatSDR JBXA9900092Water Separator · dirtyRIGHT (AIR CONDITIONING) PACK BLOWING HOT AIR ONLY ON CLIMB-OUT, AIR RETURNED TO MCO. (LEFT AIRCONDITIONING PACK INOP UNDER MEL 21-51-1). AIRCRAFT REPOSITIONED TO RDU (CREW ONLY) BOTH PACKS INOP UNDER MEL 21-51-1. REMOVED AND REPLACED NR 1 PACK WATER SEPARAJul 17, 1999 · N105ML · Fokker F28MK0100 · Humidity Control SystemSDR JBXA9900090O-Ring · failedHYDRAULIC SYSTEM NR 1 LOW QUANTITY MESSAGE, TURNED OFF PUMPS IAW MIDWAY PROCEDURE. VLANDED WITH 25 DEGREES FLAPS AND RAISED GEAR DOORS, HOWEVER NEGATIVE NOSE WHEEL STEERING. TOWED TO GATE. FOUND NR 1 ENGINE SYSTEM NR 1 HYDRAULIC PUMP QUICK DISCONNECT LINE LEJul 7, 1998 · N105ML · Fokker F28MK0100 · Hydraulic System, MainSDR JBXA980030Bleed Valve · closedRDU - FLT 17 - IN CLIMB, PACKS PRESSURE CONTROLLER PACK FAULTED, COULD NOT RESET, RETURN TO RDU. PERFORMED BITE CHECK ON PRESSURE CONTROLLER FAULTED DUE TO NR 2 ENGINE BLEED VALVE CLOSED. (M)Jan 11, 1998 · N105ML · Fokker F28MK0100 · Compressor Bleed Valve
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